SIDE STRUT LOWER SPINDLE ASSEMBLY
B
DRAG BRACE
SHOCK STRUT OUTBOARD DOOR FITTING C Wing Gear - Component Location (Details from Sht 1) Figure 102 (Sheet 2)
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A
747-400 FAULT ISOLATION/MAINT MANUAL
TRUNNION
FORK
TRUNNION
(REF)
FWD
DRAG BRACE
TRUNNION FORK
D
DRAG
LOWER BRACE
SIDE
STRUT
UPLOCK
ROLLER
INBD FWD
UPLOCK ROLLER
E
Wing Gear - Component Location (Details From Sht 1)
Figure 102 (Sheet 3)
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A
747-400 FAULT ISOLATION/MAINT MANUAL
SHOCK STRUT CHARGING VALVE SEALS
TRUCK SHIELD AND TRUCK BUMPER
Wing Gear - Component Location (Details From Sht 1)
Figure 102 (Sheet 4)
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747-400
FAULT ISOLATION/MAINT MANUAL
WING GEAR
WHEEL WELL
SEE H
UPPER
SIDE STRUT DOWNLOCK
BUNGEE
(REF)
JURY STRUT
WING GEAR
SUPPORT BEAM
(REF)
DOWNLOCK
ACTUATOR
(REF)
LOWER SIDE STRUT
TRUCK POSITIONING PRESSURE REDUCING VALVE
FWD
SIDE STRUT
TRUCK POSITIONING PRESSURE REDUCING VALVE
COMPONENT ASSEMBLY H I FROM SHT 1
Wing Gear - Component Location
Figure 102 (Sheet 5)
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A
747-400 MAINTENANCE MANUAL
WING LANDING GEAR - REMOVAL/INSTALLATION
________________________________________
1. General_______
A. This procedure contains the tasks that follow:
(1)
The removal of the wing landing gear from the airplane
(2)
The installation of the wing landing gear on the airplane.
B.
The airplane must be on jacks to do the tasks that are in this procedure.
TASK 32-11-01-004-001
2. Wing Landing Gear Removal (Fig. 401 and 402)_________________________
A. Special Tools and Equipment
(1)
8ME65B00161-1 - Drag Brace Support Strap
(2)
8ME65B01202-3 - Wing Gear Oleo Lock Assembly
(3)
G32028-116 - Wing Gear Oleo Jack (Preferred , applicable to all Airplanes)
(4)
G32028-141 Wing Gear Oleo Jack (Optional, applicable to only Airplanes with wing landing gear Outer Cylinder Gland Nut Lock Tabs facing forward)
(5)
G32028-117 Wing Gear Oleo Jack (Optional, applicable to only Airplanes with wing landing gear Outer Cylinder Gland Nut Lock Tabs facing inboard)
B.
Standard Tools and Equipment
(1)
Inclinometer
(2)
Axle jacks with adapters - 4000-pound capacity (2 required)
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